Starship / Super Heavy
RELIABILITY & S/PF/F SPLIT
REUSE CURVE
No per-reuse telemetry recorded yet. Booster-reuse rows are surfaced only when the pipeline has matched booster IDs to individual flights.
SUBSYSTEM RELIABILITY
Per-system success rates aggregated across all flights with recorded subsystem outcomes. Systems without a row are "not tracked for this vehicle yet" — we never fabricate success.
RECENT FLIGHTS
| Date | Mission | Payload | Outcome | |
|---|---|---|---|---|
| Apr 17, 2026 | Rocket Report: Starship V3 test-fired; ESA's tentative step toward crew launch | — · 100,000 kg | Success | |
| Oct 13, 2025 | Starship 38 | — · 100,000 kg | Success | |
| Jan 16, 2025 | Starship 33 | — · 100,000 kg | Partial | Briefing → |
| Jan 01, 2025 | Starship 35 | — · 100,000 kg | Failure | |
| Jan 01, 2025 | Starship 34 | — · 100,000 kg | Partial | Briefing → |
| Nov 19, 2024 | Starship 31 | — · 100,000 kg | Success | |
| Oct 13, 2024 | Starship 30 | — · 100,000 kg | Success | Briefing → |
| Jun 06, 2024 | Starship 29 | — · 100,000 kg | Success | |
| Mar 14, 2024 | Starship 28 | — · 100,000 kg | Partial | |
| Apr 20, 2023 | Starship 24 | — · 100,000 kg | Failure |
TEST HISTORY
Engine hot-fires, hop flights, tank pressurizations, captive fires, and abort events recorded against this vehicle. Every row links to its reporting source.
| Date | Test Type | Campaign / Article | Facility | Duration | Outcome | Source |
|---|---|---|---|---|---|---|
| Apr 17, 2026 | Engine Test | — | — | Success | source → | |
| May 05, 2021 | Hop Test | · SN15 | — | 6.0m | Success | source → |
| Mar 30, 2021 | Hop Test | · SN11 | — | 5.8m | Failure | source → |
| Mar 03, 2021 | Hop Test | · SN10 | — | 6.3m | Partial | source → |
| Feb 02, 2021 | Hop Test | · SN9 | — | 6.4m | Failure | source → |
| Dec 09, 2020 | Hop Test | · SN8 | — | 6.7m | Failure | source → |
| Sep 03, 2020 | Hop Test | · SN6 | — | 52.0s | Success | source → |
| Aug 04, 2020 | Hop Test | · SN5 | — | 51.0s | Success | source → |
| Aug 27, 2019 | Hop Test | — | 57.0s | Success | source → | |
| Jul 25, 2019 | Hop Test | — | 22.0s | Success | source → | |
| Apr 05, 2019 | Hop Test | — | 5.0s | Success | source → |
PAYLOAD & ORBIT MIX
OPERATOR CONTEXT
REGISTRY DATA
Source: space_launch_vehicle_registry.json · Operator page →
METHODOLOGY
Per-vehicle reliability is aggregated from the AstraVeris launch_events table with Wilson 95% lower-bound error estimates. Subsystem outcomes are extracted by a local Gemma model from primary-source articles — outcomes are never fabricated; absence of a row means "not tracked". Aspirational vehicles (not yet flown) carry registry-only metadata with explicit "Not yet flown" banners. Full specifications: /methodology/. Licensing terms: /data-licensing/.
Not investment advice. For insurance underwriting, verify against operator investigation reports.